TH-11
| Country of origin | China |
|---|---|
| Manufacturer | Space Pioneer |
| Status | Active |
| Liquid-fuel engine | |
| Propellant | LOX / RP-1 |
| Performance | |
| Thrust, vacuum | 300 kilonewtons (67,000 lbf) |
| Thrust, sea-level | 257 kilonewtons (58,000 lbf) |
| Throttle range | 50%~110% |
| Thrust-to-weight ratio | 130 |
| Chamber pressure | 10 MPa (1,500 psi) |
| Specific impulse, vacuum | 340.6s |
| Specific impulse, sea-level | 291.8s |
| Used in | |
| Tianlong-2 | |
| References | |
| Notes | [1] |
The TH-11 (Chinese:
History
[edit]Space Pioneer proposed the TH-11 engine for its Tianlong-2 launch vehicle. Full-system hot-fire tests were completed in June 2021.[2] The Tianlong-2 rocket successfully completed its maiden flight on April 2, 2023, achieving the targeted orbit. Powered by a single Tianhuo-11 engine in its second stage, this launch marked the engine's operational debut.[3]
References
[edit]- ^ "
天火 -11 -天火 系列 发动机 -天 兵科 技 ". www.spacepioneer.cc. Space Pioneer. Retrieved 13 April 2023. - ^ a b "
天 兵科 技 液体 火箭 发动机 全 系 统热试车圆满成功 ，突破 我国 航 天 多 项首创技术". finance.sina.cn. Sina. 1 June 2021. Retrieved 13 April 2023. - ^ Beil, Adrian (7 April 2023). "Chinese Tianlong-2 successfully debuts from Jiuquan". NASASpaceFlight.com. Retrieved 13 April 2023.
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| Solid fuel |
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